This document defines the requirements for a threadless, flexible, self-bonding coupling assembly, which, when installed on machined fixed cavity ferrules, provides a flexible connection for joining tubing and components in aircraft fuel, vent, or other systems. This assembled coupling, hereafter referred to as the assembly, is designed for use from -54 to 204 °C and at 862 kPa operating pressure. AS coupling components referenced herein have been qualified to AS1650. Ferrules referenced herein are inch ferrules adapted to metric tubing. MA2241 has been reaffirmed to comply with the SAE five-year review policy.
Coupling Assembly, Threadless, Flexible, Fixed Cavity, Self-Bonding, Metric
21.08.2015
Aufsatz (Konferenz)
Englisch